View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64312U 26145.30736066 +.00000000 +00000-0 +39590-3 0 00007
2 64312 70.0018 1.3378 0002639 271.1138 88.9719 14.98336013 09
| Epoch (UTC): | 25 May 2026 07:22:35 |
| Eccentricity: | 0.0002639 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3378° |
| argument of perigee: | 271.1138° |
| revolutions per day: | 14.98336013 |
| mean anomaly at epoch: | 88.9719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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